Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
S-44
IAE solid rocket engine. Used on VLS launch vehicle. First flight 1985.

Status: Active. Number: 5 . Thrust: 33.20 kN (7,464 lbf). Gross mass: 941 kg (2,074 lb). Unfuelled mass: 127 kg (279 lb). Specific impulse: 282 s. Burn time: 68 s. Height: 1.80 m (5.90 ft). Diameter: 1.00 m (3.20 ft).

Chamber Pressure: 39.50 bar. Area Ratio: 66.



Country: Brazil. Launch Vehicles: VLS, VLS-R1, VLS-1, VLM, VS-40. Propellants: Solid. Stages: S-44. Agency: IAE.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2017 Mark Wade - Contact
© / Conditions for Use